# Service difficulty reports: N772CA, cancelled Aug 8, 2013 A list on [N772CA, cancelled Aug 8, 2013](https://openairdocs.org/deregistered/N772CA-2013-08-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 78 reports - [SDR 96ZZZX3649](https://openairdocs.org/sdr/96ZZZX3649.md): Seal · defective · Jul 4, 1996 · N772CA · Doug DC862 · Turbine Engine Accessory Drive > ON RIA FLT 1712 (CDG/MIA) - DURING CRUISE AT APPROXIMATELY 1830Z, NR 4 ENGINE WAS SHUT DOWN DUE TO OIL PRESSURE LIGHT ON, ENGINE OIL PRESSURE FLUCTUATING AND DECREASING BELOW 35 PSI. AT MIA ON GROUND, MAINTENANCE FOUND LEAKING GEARBOX TOWER SHAFT SEAL. SEAL - [SDR 95ZZZZ221](https://openairdocs.org/sdr/95ZZZZ221.md): Aileron · corroded · Mar 28, 1995 · N772CA · Doug DC862 · Aileron Tabs > LEVEL 2 CORROSION, LT WING I/B AILERON O/B TAB HAS BULGING CORROSION AT FASTENERS AT I/B END LOWER SURFACE. REMOVED CORROSION AND TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 51-1-9. - [SDR 95ZZZZ220](https://openairdocs.org/sdr/95ZZZZ220.md): Skin · corroded · Mar 28, 1995 · N772CA · Doug DC862 · Ailerons > LEVEL 2 CORROSION, RT WING O/B AILERON LOWER SURFACE SKIN AT I/B END HAS CORROSION BULGING AROUND RIVETS. REMOVED CORROSION, TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW571](https://openairdocs.org/sdr/95ZZZW571.md): Support · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 7 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (W) - [SDR 95ZZZW570](https://openairdocs.org/sdr/95ZZZW570.md): Longeron · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION, LONGERON 30 LEFT IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) - [SDR 95ZZZW569](https://openairdocs.org/sdr/95ZZZW569.md): Skin · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, CORROSION BULGING OUT THROUGH FUSELAGE SKIN SURFACE AT AFT RIGHT SIDE OF FUSELAGE BS 1557R BETWEEN LONGERON 28R AND 26R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. (W) - [SDR 95ZZZW568](https://openairdocs.org/sdr/95ZZZW568.md): Support · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 12 INCHES LBL. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (W) - [SDR 95ZZZW535](https://openairdocs.org/sdr/95ZZZW535.md): Skin · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Horizontal Stabilizer, Plate/Skin > LEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LOWER SURFACE SKI AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-2. (W) - [SDR 95ZZZW534](https://openairdocs.org/sdr/95ZZZW534.md): Window Frame · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, WINDOW NR 23R HAS CORROSION INSIDE FRAME. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH EO 9402289. - [SDR 95ZZZW533](https://openairdocs.org/sdr/95ZZZW533.md): Skin · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Horizontal Stabilizer, Plate/Skin > LEVEL 2 CORROSION, RT HORIZONTAL STAB UPPER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 55-3-0. (W) - [SDR 95ZZZW532](https://openairdocs.org/sdr/95ZZZW532.md): Skin · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, FUSELAGE RT SIDE EXTERIOR SKIN FRAMES 670 TO FS 685 HAS SKIN CRACK AND BULGING AROUND FASTENER HEADS LGRN 21R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH DWG RCH D85330-5018. (W) - [SDR 95ZZZW531](https://openairdocs.org/sdr/95ZZZW531.md): Skin · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Horizontal Stabilizer, Plate/Skin > LEVEL 2 CORROSION, RT HORIZONTAL STABILIZER LOWER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-1. (W) - [SDR 95ZZZW530](https://openairdocs.org/sdr/95ZZZW530.md): Spar Cap · corroded · Mar 3, 1995 · N772CA · Doug DC862 · Wing Spar > LEVEL 2 CORROSION RT WING LEADING EDGE UPPER AT FRONT SPAR CAP ATTACH FLANGE HAS CORROSION AROUND SCREW HEADS OUTBOARD OF NR 4 PYLON FROM APPROXIMATELY XFS 503 TO XFS 710. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. - [SDR 95ZZZW548](https://openairdocs.org/sdr/95ZZZW548.md): Skin · corroded · Mar 2, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, AFT CABIN FUSELAGE SKIN IS CORRODED BETWEEN BS 1586L AND 1574, LONGERON 26L AND LONGERON 24L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. - [SDR 95ZZZW567](https://openairdocs.org/sdr/95ZZZW567.md): Longeron · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION, AFT FUSELAGE LONGERON 24R BETWEEN FS 1500 AND 1480 HAS SURFACE CORROSION AND BULGES. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) - [SDR 95ZZZW566](https://openairdocs.org/sdr/95ZZZW566.md): Skin · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, FUSELAGE LOWER LOBE SKIN IS CORRODED AT CENTER PRESSURE BULKHEAD VERTICAL SUPPORT 4 INCHES LBL BETWEEN BS 1606 AND 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) - [SDR 95ZZZW565](https://openairdocs.org/sdr/95ZZZW565.md): Window Frame · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, AFT FUSELAGE MAIN CABIN WINDOW FRAME FOR WINDOW 19R HAS CORROSION ON INSIDE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW RICH DRAWING 5164-6. (W) - [SDR 95ZZZW547](https://openairdocs.org/sdr/95ZZZW547.md): Skin · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, AFT MAIN CABIN LOWER FUSELAGE SKIN IS CORRODED FROM BS 1530 TO BS 1606 LONGERON 35L TO 35R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. - [SDR 95ZZZW546](https://openairdocs.org/sdr/95ZZZW546.md): Slot Door · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Trailing Edge Flaps > LEVEL 2 CORROSION, LEFT WING NR 1 SLOT DOOR HAS DOUBLER REPAIR THAT IS SURROUNDED BY CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER DOUGLAS FILE NR 258324. - [SDR 95ZZZW545](https://openairdocs.org/sdr/95ZZZW545.md): Flange · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Wing Miscellaneous Structure > LEVEL 2 CORROSION, LEFT AUXILLARY TANK UPPER ATTACH FLANGE HAS INTERGRANULAR CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. - [SDR 95ZZZW544](https://openairdocs.org/sdr/95ZZZW544.md): Support · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, AFT CABIN TRIANGLE FLOOR WEB SUPPORT IS CORRODED AT BS 1574 CENTER, CENTER LINE 12 INCHES LBL 12 INCHES RBL. REMOVED AND REPLACED TRIANGLE FLOOR WEB PER SRM 53-1-0. - [SDR 95ZZZW543](https://openairdocs.org/sdr/95ZZZW543.md): Frame · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Main, Frame > LEVEL 2 CORROSION, AFT CABIN CIRCUMFERENTIAL FRAME IS CORRODED AT BS 1574L FROM LONGERON 24 TO 26L. REMOVED CORROSION AND REPLACED FRAME SECTION PER SRM 53-1-0. - [SDR 95ZZZW542](https://openairdocs.org/sdr/95ZZZW542.md): Floor Beam · corroded · Mar 1, 1995 · N772CA · Doug DC862 · Fuselage Main, Floor Beam > LEVEL 2 CORROSION, AFT CABIN FLOOR BEAM CAP AT BS 1540 IS CORRODED FROM 45 INCHES LBL TO 45 INCHES. REMOVED AND REPLACED FLOOR BEAM CAP PER SRM 53-1-0. - [SDR 95ZZZW539](https://openairdocs.org/sdr/95ZZZW539.md): Floor Beam · corroded · Feb 24, 1995 · N772CA · Doug DC862 · Fuselage Main, Floor Beam > LEVEL 2 CORROSION, ENTIRE FLOOR BEAM CAP AT BS 1586 IS CORRODED FROM LEFT TO RIGHT SIDE OF CABIN. CLEANED CORROSION, FABRICATED, AND INSTALLED NEW FLOOR BEAM PER SRM 53-1-0. - [SDR 95ZZZW538](https://openairdocs.org/sdr/95ZZZW538.md): Fitting · corroded · Feb 24, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, LONGERON 32 RIGHT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW537](https://openairdocs.org/sdr/95ZZZW537.md): Fitting · corroded · Feb 24, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, AFT CARGO COMPARTMENT BATHTUB FITTING IS CORRODED AT BS 1530R, LONGERON 30R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW536](https://openairdocs.org/sdr/95ZZZW536.md): Skin · corroded · Feb 24, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, FUSELAGE SKIN CORRODED BETWEEN BS 1530 AND BS 1540 BETWEEN LONGERON 36 AND LONGERON 34 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) - [SDR 95ZZZZ153](https://openairdocs.org/sdr/95ZZZZ153.md): Support · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 9 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ152](https://openairdocs.org/sdr/95ZZZZ152.md): Longeron · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION/LONGERON 26 LEFT END FITTING IS CORRODED AT BS 1530 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ151](https://openairdocs.org/sdr/95ZZZZ151.md): Support · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1480L AND BS 1520L, 15 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ150](https://openairdocs.org/sdr/95ZZZZ150.md): Fitting · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/LONGERON 30 RIGHT END FITTING IS CORRODED AT BS 1530 RIGHT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ149](https://openairdocs.org/sdr/95ZZZZ149.md): Support · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 22 INCHES RBL. REMOVED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ148](https://openairdocs.org/sdr/95ZZZZ148.md): Support · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CABIN SQUARE FLOOR SUPPORT FRAME IS CORRODED BETWEEN BS 1586 AND BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ147](https://openairdocs.org/sdr/95ZZZZ147.md): Window · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Passenger Compartment Windows > LEVEL 2 CORROSION/MAIN CABIN WINDOW NR 18R HAS CORROSION ON INSIDE SURFACE OF FRAME. FABRICATED AND INSTALLED REPAIR PER RICH REPAIR SKETCH 5164-6. - [SDR 95ZZZZ146](https://openairdocs.org/sdr/95ZZZZ146.md): Web · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT CIRCUMFERRENTIAL WEB CORRODED AT BS 1540 FROM 34L TO 34R. REMOVED CORROSION AND REPLACED SPLICE PLATE PER SRM 51-1-0. - [SDR 95ZZZZ145](https://openairdocs.org/sdr/95ZZZZ145.md): Floor Support · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT OVERHEAD FLOOR SUPPORT CORRODED BETWEEN BS 1460 AND BS 1500, 12 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZZ144](https://openairdocs.org/sdr/95ZZZZ144.md): Angle · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT ANGLE AT BS 1520 IS CORRODED FROM 12 INCHES RBL TO 45 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW242](https://openairdocs.org/sdr/95ZZZW242.md): Frame · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Frame > LEVEL 2 CORROSION, CIRCUMFERRENTIAL FRAME IS CORRODED AT BS 1574 BETWEEN LONGERON 24 RT AND 26 RT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. - [SDR 95ZZZW241](https://openairdocs.org/sdr/95ZZZW241.md): Fitting · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, LONGERON 30 LT END BATHTUB FITTING IS CORRODED AT BS 1606L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW240](https://openairdocs.org/sdr/95ZZZW240.md): Frame · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Frame > LEVEL 2 CORROSION, AFT CABIN LOWER CIRCUMFERRENTIAL FRAME 'J' FLANGES ARE CORRODED, UPPER AND LOWER AT BS 1586 FROM LONGERON 24L TO 24R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. - [SDR 95ZZZW239](https://openairdocs.org/sdr/95ZZZW239.md): Floorbeam · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Floor Beam > LEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP AT BS 1574 IS CORRODED FROM 36 INCHES LBL TO 36 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW238](https://openairdocs.org/sdr/95ZZZW238.md): Longeron · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION, LONGERON 36 IS CORRODED AT BS 1550. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI ER SRM 53-2-2. - [SDR 95ZZZW237](https://openairdocs.org/sdr/95ZZZW237.md): Longeron · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION, LONGERON 36 IS CORRODED 6 INCHES FWD AND AFT OF BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. - [SDR 95ZZZW236](https://openairdocs.org/sdr/95ZZZW236.md): Longeron · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION, LONGERON 36 IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. - [SDR 95ZZZW235](https://openairdocs.org/sdr/95ZZZW235.md): Longeron · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Longeron/Stringer > LEVEL 2 CORROSION, LONGERON 32 RT IS CORRODED BETWEEN BS 1606 AND 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. - [SDR 95ZZZW234](https://openairdocs.org/sdr/95ZZZW234.md): Floorbeam · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Main, Floor Beam > LEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP IS CORRODED AT BS 1440 FROM 45 INCHES LBL TO 45 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW233](https://openairdocs.org/sdr/95ZZZW233.md): Fitting · corroded · Feb 22, 1995 · N772CA · Doug DC862 · Fuselage Miscellaneous Structure > LEVEL 2 CORROSION, LONGERON 30 RT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. - [SDR 95ZZZW253](https://openairdocs.org/sdr/95ZZZW253.md): Seat Track · corroded · Feb 10, 1995 · N772CA · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 150 RT TO BS 1540 RT, 39 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA, TREATED, PRIMED AND INSTALLED REPAIR AS PER SRM 51-10-00 AND 51-1-8. - [SDR 95ZZZW252](https://openairdocs.org/sdr/95ZZZW252.md): Seat Track · corroded · Feb 10, 1995 · N772CA · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 1500 RT TO BS 1540 RT 25 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA TREATED, PRIMED AND INSTALLED REPAIR AS PER SRM 51-1-8 AND 51-10-0. - [SDR 95ZZZW251](https://openairdocs.org/sdr/95ZZZW251.md): Skin · corroded · Feb 10, 1995 · N772CA · Doug DC862 · Fuselage Main, Plate/Skin > LEVEL 2 CORROSION, FUSELAGE RT EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. REMOVED WINDOW, REMOVED CORROSION, FABRICATED REPAIR, TREATED, PRIMED AND INSTALLED REPAIR AND WINDOW AS PER SRM 51-1-8, DRAWING RCH D85310-5015 AND MM 56-20-00. Next page: https://openairdocs.org/deregistered/N772CA-2013-08-08/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N772CA' AND deregistration_id = 'N772CA-2013-08-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N772CA-2013-08-08/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.